25   Artículos

 
en línea
Georgia Korompili, Günter Mußbach and Christos Riziotis    
In the realm of space exploration, solid rocket motors (SRMs) play a pivotal role due to their reliability and high thrust-to-weight ratio. Serving as boosters in space launch vehicles and employed in military systems, and other critical & emerging a... ver más
Revista: Instruments    Formato: Electrónico

 
en línea
Zhuopu Wang, Kairui Yu and Yuanzhe Liu    
The unsteady combustion of solid propellants under oscillating environments is the key to understanding the combustion instability inside solid rocket motors. The discontinuous Galerkin?finite element method (DG-FEM) is introduced to provide an efficient... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Stefano Mini, Fabrizio Ponti, Alessandro Brusa, Roberto Bertacin and Barbara Betti    
Numerical studies intended to predict solid rocket motors anomalies are the major contributors when developing strategies to both limit expensive fire tests and to investigate and understand the physical phenomena from which anomalies can arise. This pap... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhihong Wang, Chunguang Wang and Weiping Tian    
In order to study the flow characteristics of a nozzle with large expansion ratio and its influence on the force on the nozzle, ground cold flow test research and a fluid?structure coupling simulation analysis were carried out (maximum expansion ratio e ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Zhuopu Wang, Wenchao Zhang and Yuanzhe Liu    
Solid rocket motors are prone to combustion instabilities, which may lead to various problems for the rockets, from unexpected oscillations, precision decreasing, to explosion. The unsteady combustion dynamics of the propellants play a crucial role in mo... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Songchen Yue, Lu Liu, Huan Liu, Yanfeng Jiang, Peijin Liu, Aimin Pang, Guangxue Zhang and Wen Ao    
Solid propellant combustion and flow are significantly affected by condensed combustion products (CCPs) in solid rocket motors. A new aluminum agglomeration model is established using the discrete element method, considering the burning rate and formulat... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Weiqiang Xiong, Yunjie Liu, Tianfu Zhang, Shixi Wu, Dawen Zeng, Xiang Guo and Aimin Pang    
Aluminium?lithium alloy (Al?Li alloy) powder has excellent ignition and combustion performance. The combustion product of Al?Li alloy powder combined with ammonium perchlorate is gaseous at the working temperature of solid rocket motors, which greatly re... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Shixiong Song, Quanbin Ren, Min Tang, Jiawei Shi and Jiawei Wang    
Fused deposition technology (FDM), as an additive manufacturing (AM) technology, holds immense potential in the field of solid grain manufacturing. It can accomplish complex grain shaping with ultra-low-pressure ratios, which are challenging to achieve u... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Jihyoung Cha    
This study deals with the mathematical modeling and numerical simulation of chemical propulsion systems (CPSs). For this, we investigate and summarize a comprehensive collection of the simulation modeling developments of CPSs in academic works, applicati... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Hui Tian, Zhongshuo Wang, Hao Zhu, Yudong Lu, Jingfei Gao and Guobiao Cai    
Catalytic hybrid rocket motors using hydrogen peroxide (HP) are easy and efficient to achieve multiple starts and stops, and hydroxyl-terminated polybutadiene (HTPB) grains are commonly used due to their excellent mechanical properties. The low regressio... ver más
Revista: Applied Sciences    Formato: Electrónico

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